Maximum Take-Off Weight
5.1 t (paragliders: kg)
Pictures
No pictures yet for this family.
Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Soko J-21 Jastreb |
5.1 |
275 |
1.52 |
Similar airplanes
All data (25 fields)
- Name
- Soko J-21 Jastreb
- Manufacturer
- SOKO
- Description
- The Soko J-21 Jastreb (from ), referred to as the J-1 Jastreb in some sources, is a Yugoslav single-seat, single-engined, light attack aircraft, designed by the Aeronautical Technical Institute (ATI) and Military Technical Institute (VTI), in Belgrade, and manufactured by SOKO in Mostar.
- ICAO Code
- JAST
- First Flight
- 1965-07-19
- Production End
- 1977-01-01
- Designer
- Aeronautical Technical Institute (ATI)
- Type
- Light attack aircraft
- Length (m)
- 10.88
- Height (m)
- 3.64
- Cockpit Crew
- 1
- Max Speed (km/h)
- 820
- Cruise Speed (km/h)
- 740
- Max Ceiling (m)
- 12000
- Rate of Climb (m/s)
- 21
- Armament
- 3 × 0.5 in Browning AN/M3 machine guns; ; 2 × 250 kg general-purpose bombs or; 2 × 150 kg cluster bombs or; 2 × 120 kg cluster fragmentation bombs; 6 × VRZ-157 127 mm rockets; 8
- Number Built
- 224
- Powerplant Description
- 1 × BMB (Rolls-Royce/Bristol Siddeley) Viper Mk 531 turbojet engine, 13.32 kN thrust each
- Primary Users
- Yugoslav Air Force
- Status
- Retired from Republika Srpska Air Force (2006)
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Soko_J-21_Jastreb
- Flat Wing Span (m)
- 10.56
- Flat Wing Area (m²)
- 19.43
- Wake Category
- L
- Number of Engines
- 1